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WO/2023/057377A9 |
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part re...
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WO/2024/087990A1 |
An aircraft and a control surface hinge structure thereof. The hinge structure comprises a stabilizer hinge (1) and a movable-surface hinge (2), which are arranged opposite each other, wherein the stabilizer hinge (1) comprises a stabili...
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WO/2024/091205A1 |
The present invention relates to a body (2) on an air vehicle; at least one wing (3) located on the body (2), extending outward from the body (2), allowing the air vehicle to rise depending on the air flow; at least one flap (4) that is ...
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WO/2024/068661A1 |
A control unit (6, 7) is indicated for controlling the pitch of an aircraft (1), the control unit (6, 7) comprising at least one adjustable control element (6) and an adjustment mechanism (7) for actively adjusting the at least one contr...
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WO/2024/060633A1 |
An aircraft wing (10) having an integrated distributed ducted fan, the aircraft wing (10) being attached to a fuselage (20) and being provided with a ducted fan power set (30), wherein the ducted fan power set (30) is provided on an inbo...
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WO/2024/058619A1 |
The present invention relates to an airship capable of easily switching directions, the airship comprising an aerial vehicle (mother ship) formed in a disc or polygonal shape provided with a jet engine, a rotating body having a jet engin...
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WO/2024/052505A1 |
The invention relates to a wing arrangement (10) that comprises a main wing (12) and a slat (14) mounted to the main wing in front of the main wing (12) and counter to a direction of flow. A gap (16) with a flow inlet (18) and a flow out...
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WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
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WO/2024/012942A1 |
The present invention relates to an adjustable guide bushing (10) comprising a first bushing (20) with a first eccentric opening (30) and a second bushing (40) with a second eccentric opening (50), wherein the first bushing (20) is accom...
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WO/2024/003642A1 |
A ducted wing is configured to be connected to an aircraft. The ducted wing includes an array of integrated jetfoils. Each jetfoil includes a propulsor fan, an upper wing portion, and a lower wing portion that extends past an end of the ...
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WO/2023/220311A1 |
An ejector system is constructed of a soft yet strong material such as silicone-based material which can be pressed to conform within a small space and stowed when inactive and can be expanded or stretched by mechanical, pneumatic or hyd...
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WO/2023/198267A1 |
An aerodynamic profile for an aircraft, comprises a core (6, 7, 8) made of foam, a skin (11, 12) defining an outer surface of the wing and cloths (14) forming spars and/or ribs. The profile a wing, a canard, a horizontal stabiliser, a ve...
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WO/2023/135037A1 |
The invention relates to a movable leading-edge flap (16) comprising an aerodynamic part (19) and at least one drive and guide rail system (42), which system includes two rails (44) each extending over the entire length of the rail syste...
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WO/2023/122717A1 |
A method of operating an aircraft including takeoff of an aircraft; transitioning the aircraft to a forward flight configuration by increasing an amount of forward propulsive force generated by a propeller assembly from equal to or less ...
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WO/2023/109154A1 |
Disclosed are a wing and a method for improving control efficiency of a two-dimensional airfoil rudder surface. According to the technical solution, an original symmetric airfoil rudder surface is transformed into an asymmetric airfoil r...
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WO/2023/099117A1 |
The invention relates to a device comprising an asymmetrical wing profile (2) and an adjusting device (15), which asymmetrical wing profile (2) has a profile thickness (q) and a profile chord (p) extending between a wing leading edge (n)...
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WO/2023/077686A1 |
An aircraft flap (10) that excludes an actuation structure providing an air jet. The aircraft flap comprises at least one side-edge opening that is connected to one or more air channels for directing an airflow in and/or out to reduce th...
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WO/2023/034302A9 |
A system and method for lift augmentation of an aircraft having a wing with a leading edge and a trailing edge extending along a wingspan, a plurality of thrust-producing devices connected to the bottom of said wing, at least one flap co...
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WO/2023/057377A1 |
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part re...
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WO/2023/055320A1 |
The present invention relates to a sensor unit (2) located on an air vehicle, which enables the measurement of air speed, engine torque and lateral acceleration of the air vehicle; a flight control computer (3) which enables a first adju...
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WO/2023/043313A1 |
Actuation device for a high-lift device of a rotor blade, comprising a first link, movable in a span- wise direction, outwardly by a centrifugal force, a biasing member, connected with the first link and configured to exert an opposite f...
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WO/2023/037120A1 |
The present disclosure relates to a foldable moveable member for an air vehicle. The moveable member comprises a sheet, the sheet comprising a first portion, a second portion, and a fold region. The first portion is connected to the seco...
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WO/2023/019160A1 |
A bearing system for a control surface of a high speed flight vehicle includes a bearing configured to support the control surface, and a pressurized lubricant chamber containing a lubricant for the bearing. The lubricant contained in th...
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WO/2022/260894A1 |
The present disclosure is drawn to an aircraft wing assembly that can include an airfoil including a leading edge, a first slat positioned or positionable upwind relative to the leading edge leaving a first airflow gap between the first ...
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WO/2022/249758A1 |
A front edge high lift device according to one aspect of the present invention can be deployed/stored with respect to a main wing front edge of an aircraft, and comprises a slat body and a buffer part. The slat body has: a front edge par...
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WO/2022/243113A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated such that it sequentially adopts a plurality of different partial load sharing modes in a time variable manner, which provide for...
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WO/2022/243112A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated in at least one normal operation mode such that it provides for load sharing across electrical power sources (A, B, C, D) with re...
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WO/2022/239574A1 |
A leading edge high-lift device according to one embodiment of the present invention can be expanded and stored in relation to a mother wing leading edge and comprises: a leading edge part; a trailing edge part forming a gap with the mot...
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WO/2022/235145A1 |
The invention relates to aviation equipment. An object of this invention is to develop a new device, which can extend the range of aerodynamic devices for aviation, increase the efficiency of the air flow power use around the wing, and i...
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WO/2022/212247A1 |
In an aspect a system for fly-by-wire flight control configured for use in electric aircraft includes at least a sensor, wherein the sensor is communicatively connected a pilot control and configured to detect a pilot input from the pilo...
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WO/2022/204278A1 |
Wind turbine blades and wind turbine systems that include a co-flow jet are described. An example wind turbine blade has a main body and a fluid pressurizer. The main body has a. first portion, a second portion, a leading edge, a trailin...
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WO/2022/198285A1 |
A longitudinal control surface (30) for an aircraft (10) is described, in particular a turboprop/propfan aircraft with engines (12) mounted on the rear of the fuselage (11). This longitudinal control surface (30) is positioned in the str...
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WO/2022/175065A1 |
The invention refers to an aircraft (1, 3), particularly an aircraft (1, 3) capable of vertical take-off and landing, comprising a fuselage (3, 4), and a variable lift body (5, 7) defining an aerofoil (51, 53) and being moveably attached...
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WO/2022/175099A1 |
The present invention relates to an integrated controller unit (10) for controlling at least one engine motor (26) and at least one servo motor (28), comprising a power link section (12) for connecting the controller unit (10) to an exte...
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WO/2022/175106A1 |
A flight control system (10) for an aircraft comprises a flight control computer system (12), which is connected via an electronic or optoelectronic bus system (22) with a plurality of bus nodes (14, 16, 18, 20), which each are configure...
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WO/2022/175071A1 |
The present invention relates to a wing assembly (10) for an aircraft with a fuselage and at least one pair of wings, the wing assembly (10) defining a direction of flow (F) with respect to which the wing assembly (10) is configured to c...
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WO/2022/166813A1 |
Disclosed are an aircraft and a control method for an aircraft. The aircraft comprises an empennage (10), the empennage (10) comprising an empennage body (101), a left tail vane (102) and a right tail vane (103), wherein the left tail va...
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WO/2022/140362A1 |
The disclosed embodiments are directed to a modular autonomous vehicle system comprising a blended wing body module, at least two high speed long range wing panel modules configured to interchangeably mount to the blended wing body modul...
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WO/2022/104273A1 |
During landing and rejected-takeoff flight phases, aircraft drag is a useful force to supplement braking and reduce stopping distance. During descents, aircraft drag is a useful force in steepening flight path angle and achieving higher ...
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WO/2022/087607A1 |
An aircraft with a variety of control surfaces including but not limited to multiple winglet rudders. Each winglet can have multiple independently controlled rudders to improve the flight stability and maneuverability of the aircraft. Ad...
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WO/2022/066001A1 |
An aircraft wing (1) provided with a trailing edge region (2) which is provided with a noise attenuation structure, which at least comprises in combination, looking in an upwards direction: a first micro perforated plate (2.1) with micro...
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WO/2022/061021A1 |
A multi-segment oblique flying wing aircraft which has three distinct segments including two outer wing segments and a central wing segment. The central segment may be thicker in the vertical direction and adapted to hold pilots and pass...
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WO/2022/036433A1 |
A system for providing a simple, safe and inexpensive mechanism to provide flight control in an aircraft. In one embodiment, an anti-torque system (20) for a rotary-wing aircraft has an airfoil (22) with a first surface (24) extending fr...
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WO/2022/034272A1 |
Disclosed is an aircraft capable of vertical takeoff and landing in high wind conditions. The invention relates to a device allowing an aircraft in flight, capable of vertical takeoff and landing (VTOL) and having wings oriented vertical...
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WO/2022/023790A1 |
The design of a modern multi-purpose actuator with the capability of performance similar to flight control surfaces that leads to optimal utilization of ambient airflow and is applied as an auxiliary system in case of failure of the main...
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WO/2022/024112A1 |
Refueling devices for use in in-flight refueling operation are provided, including a body configured for being towed by a tanker aircraft and having a boom member that has a fuel delivery nozzle, a spatial control system and a longitudin...
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WO/2022/019856A1 |
This invention relates to a body (2), at least one control surface (3) located on the body (2), enabling to control the flow of fluid by moving relative to the body (2), at least one actuator (4) produced from an electro-active polymer m...
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WO/2022/019857A1 |
The present invention relates to at least one body (2) provided in air vehicles; at least one wing flap (3) which allows the air flow to be controlled by moving relative to the body (2) located thereon, thus allows the air vehicle to man...
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WO/2022/019852A1 |
The invention relates to a body (2), at least one actuator (3) produced from an electro¬ active polymer material that changes form due to electrical energy, thereby actuating the body (2), at least two strengtheners (4) allowing the act...
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WO/2022/019854A1 |
This invention relates to a body (2) located in an air and/or space vehicle, at least one control surface (3) which is located on the body (2) and which by moving relatively to the body (2), enables air flow to be controlled and the air ...
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